Title:
流体輸送システムの複合管
Document Type and Number:
Japanese Patent JP6633672
Kind Code:
B2
Abstract:
A method and apparatus for reducing an intensity of an electrical discharge that occurs within a fluid transport system in an aerospace vehicle. The aerospace vehicle is operated. The fluid transport system in the aerospace vehicle is comprised of materials selected such that the fluid transport system has an electrical configuration. The intensity of the electrical discharge that occurs within the fluid transport system during operation of the aerospace vehicle is reduced to within selected tolerances by the electrical configuration of the fluid transport system.
Inventors:
Gau, Kevin O'Brien
Kelly, Nathan Michael
Axtel, John Thomas
Irwin, James Patrick
Mintia, David William
Velasco, Diego A.
Johnson, Benjamin A.
Kelly, Nathan Michael
Axtel, John Thomas
Irwin, James Patrick
Mintia, David William
Velasco, Diego A.
Johnson, Benjamin A.
Application Number:
JP2018053923A
Publication Date:
January 22, 2020
Filing Date:
March 22, 2018
Export Citation:
Assignee:
The Boeing Company
International Classes:
F16L25/01; B64D37/32; F16L9/00; F16L23/06; H05F3/02
Domestic Patent References:
| JP2010126133A | ||||
| JP2007500827A |
Foreign References:
| US20120056416 | ||||
| WO2012032406A2 | ||||
| US20100122749 |
Attorney, Agent or Firm:
Sonoda/Kobayashi Patent Business Corporation